Miniaturized MEMS Based Integrated Navigation High Precision MEMS INS Customized MS- 5222X

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xProduct Name | MEMS Based Integrated Navigation | Grade | Industrial |
---|---|---|---|
Applications | Aerospace, Defense, Navigation, Robotics | Customized Support | OEM, ODM |
Highlight | Miniaturized MEMS Based Integrated Navigation,MEMS Based Integrated Navigation High Precision,MEMS INS Customized |
MS- 5222X Miniaturized High - Precision MEMS Integrated Navigation System
MS- 5222X is a miniaturized high - precision MEMS integrated navigation system with built-in self-developed high-precision MEMS IMU (inertial measurement unit) and self-developed high-precision GNSS module. It adopts multi-source Kalman filter fusion algorithm to provide continuous and reliable high-precision positioning and navigation information in complex environments. The product is widely used in UAV, surveying and mapping, stable platform, satellite communication and other fields.
Key Features:
Support BDS, GPS, GLONASS, Galileo and QZSS full system multi-frequency points, support Beidou three satellite systems All IMUs are factory-calibrated for temperature and dynamic calibration Optimized SWaP-C design, small and multifunctional Supports multiple alignment methods such as transfer alignment and dynamic alignment
High reliability product design, scientific and effective product development Professional and complete production equipment, strict quality control production process Deliver better products to users
Many years of industry application experience and practical cases of over a thousand industry users Industry-leading compensation calibration technology, efficient and fast professional technical response Provide users with more satisfactory services
Specifications:
Indicator |
Specifications (typical values) |
Remark |
|
Startup time |
Integrated navigation alignment time |
<60s |
Requires open environment Including GNSS cold start 25s , RTK initialization 5s |
Satellite signal tracking capability |
Frequency |
BDS B1I/B2I/B3I , GPS L1/L2/L5 GLONASS L1/L2, GALILEO E1//E5a/E5b, QZSS L1/L2/L5 |
|
Heading accuracy |
Single Antenna |
0.2° |
Need to be maneuverable |
Maintaining accuracy |
0.15°/min |
GNSS failure |
|
Attitude accuracy |
GNSS effective |
0.1° |
RTK/ single point dual frequency |
Maintaining accuracy |
0.15°/min |
GNSS failure |
|
Horizontal positioning accuracy |
GNSS effective |
1.2m |
Single point dual frequency |
1cm + 1ppm |
RTK |
||
Horizontal speed accuracy |
GNSS effective |
0.03m/s |
RTK/single point dual frequency |
Timing accuracy |
GNSS effective |
20ns |
|
Gyroscope |
Measuring range |
±1000°/s |
|
Bias instability |
2°/h |
Allan variance |
|
Scale factor nonlinearity |
200ppm |
|
|
Accelerometer |
Measuring range |
±16g |
|
Bias instability |
0.02mg |
Allan variance |
|
Scale factor nonlinearity |
200ppm |
±1 g |
|
Data update rate |
GNSS data results |
10Hz |
Positioning / speed / heading information |
IMU Raw Data |
200Hz |
|
|
Combined navigation solution results |
200Hz |
|
|
Electrical Characteristics |
Communication interface |
RS-422 * 1 , LVTTL * 2 |
|
Voltage |
5V DC ± 5% |
|
|
Power consumption |
≤ 2W |
|
|
Structural characteristics |
size |
46*46*11.5 mm |
Dimensions without antenna interface |
weight |
≤ 100 g |
|
|
Usage Environment |
Operating temperature |
-40℃ ~ +75℃ |
|
Storage temperature |
-55℃ ~ +95℃ |
|
|
vibration |
6.06g ( 20~2000 Hz ) |
|
|
Shock |
40g / 11ms |
|
|
Note: All indicators without statistical methods are RMS statistics; 231012 and later versions support up to 200 Hz , and firmware prior to 231012 supports up to 100 Hz . |